Integral Spring Junction

ABSTRACT

Spinal stabilization devices, systems and methods are provided that include a spring junction wherein a structural member is mountable to a spine attachment fastener and a resilient element is affixed to the structural member along an attachment region of the resilient element. The attachment region is disposed physically separately with respect to an active region of the resilient element. The attachment region can include a weld region produced via an E-beam welding process involving temperatures of 1000° F. or greater, wherein a heat-affected zone adjacent the weld region is disposed physically separately with respect to the active region. The resilient element may be a coil spring including bend regions adjacent its outermost (i.e., last) coils wherein the material of the coil spring initially bends away from the last coil, then bends back toward the last coil before terminating near the last coil.

CROSS-REFERENCE TO RELATED APPLICATION

The present application is a continuation application that claimspriority benefit to a co-pending and commonly assigned non-provisionalpatent application entitled “Spring Junction and Assembly Methods forSpinal Device,” which was filed on Aug. 3, 2005, and assigned Ser. No.11/196,102.

BACKGROUND

1. Technical Field

The present disclosure relates to advantageous devices, systems andmethods for spinal stabilization. More particularly, the presentdisclosure relates to devices, systems and methods for providing dynamicstabilization to the spine with systems/devices that include one or moreenhanced spring junctions so as to provide clinically efficaciousresults.

2. Background Art

Each year, over 200,000 patients undergo lumbar fusion surgery in theUnited States. While fusion is effective about seventy percent of thetime, there are consequences even to these successful procedures,including a reduced range of motion and an increased load transfer toadjacent levels of the spine, which may accelerate degeneration at thoselevels. Further, a significant number of back-pain patients, estimatedto exceed seven million in the U.S., simply endure chronic low-backpain, rather than risk procedures that may not be appropriate oreffective in alleviating their symptoms.

New treatment modalities, collectively called motion preservationdevices, are currently being developed to address these limitations.Some promising therapies are in the form of nucleus, disc or facetreplacements. Other motion preservation devices provide dynamic internalstabilization of the injured and/or degenerated spine, e.g., the Dynesysstabilization system (Zimmer, Inc.; Warsaw, Ind.) and the Graf Ligament.A major goal of this concept is the stabilization of the spine toprevent pain while preserving near normal spinal function.

To provide dynamic internal spinal stabilization, motion preservationdevices may advantageously include dynamic junctions that exhibitmultiple degrees of freedom and commonly include activeforce-absorbing/force-generating structures. Such structures may includeone or more resilient elements, e.g., torsion springs and/or coilsprings, designed and deployed so as to contribute strength andflexibility to the overall device. While the flexibility afforded bysuch resilient elements is plainly critical to the effectiveness of therespective devices of which they faun a part, the elevated force levelsassociated with the use of such resilient elements can result in suchresilient elements developing significant levels of internal stress.Depending on the magnitude and location thereof, internal stresses maypose the potential for stress-induced fatigue, material deformationand/or cracks. The FDA has promulgated rules (e.g., Title 21, SubchapterH, Part 888, Subpart D, Section 888.3070 regarding pedicle screw spinalsystems) that, in relevant part, require manufacturers to demonstratecompliance with special controls, including but not limited toapplicable mechanical testing standards geared toward high reliabilityand durability.

With the foregoing in mind, those skilled in the art will understandthat a need exists for devices, systems and methods formotion-preserving spinal stabilization devices and systems havingreliable, durable constructions. In addition, a need exists formanufacturing processes and/or techniques that may be used to reliablyand efficiently produce motion-preserving spinal stabilization devicesand systems. These and other needs are satisfied by the discloseddevices and systems that include advantageous spring junctions, as wellas the associate methods for manufacture/assembly thereof.

SUMMARY OF THE PRESENT DISCLOSURE

According to the present disclosure, advantageous devices, systems andmethods for spinal stabilization are provided. According to exemplaryembodiments of the present disclosure, the disclosed devices, systemsand methods include a spring junction that promotes reliable andefficacious spinal stabilization. The disclosed spring junction includesa structural member that is mounted or mountable with respect to a spineattachment fastener such as a pedicle screw, and a resilient elementaffixed to the structural member. The resilient element has anattachment region, along which the resilient element is affixed to thestructural member, and an active region. The attachment region of theresilient element is physically separately disposed with respect to theactive region thereof.

According to exemplary embodiments of the present disclosure, the springjunction includes a weld region. A heat-affected zone of the resilientelement and associated with the weld region is disposed adjacent theweld region, but is physically separately disposed with respect to theactive region of the resilient element. The active region of theresilient element is generally subjected to cyclical stress, e.g.,during in situ use of the disclosed spinal stabilization device. Inexemplary embodiments, the weld region is produced via a weldingprocess, such as electron-beam welding, and accordingly may be subjectedto welding temperatures of about 1000° F. or higher. In addition, inexemplary embodiments of the present disclosure, the resilient elementtakes the form of a spring, e.g., a coil spring or helical spring, whichextends into the weld region and which is mounted with respect to thestructural member to form the spring junction.

According to further exemplary embodiments of the present disclosure,the resilient element includes a bend region disposed between the weldregion and an adjacent coil of the resilient element that extends alonga helically-shaped path. The bend region is sized and shaped so as toinitially bend away from the helically-shaped path before bending backtoward the helically-shaped path and terminating at or in the weldregion. In some such embodiments, the direction of the initial bend awayfrom the helically-shaped path includes an axial component, but does notinclude a radial component. The bend region may further be sized andshaped so as to remain substantially peripherally aligned with suchhelically-shaped path when viewed in an axial direction with respect tothe helically-shaped path. Of note, such spring junctions may be formedat opposite ends of the resilient element such that the resilientelement/spring is mounted between spaced-apart structural members thatare permitted to move relative to each other.

According to further exemplary embodiments of the present disclosure, arod is mounted with respect to (or integrally formed with) thestructural member. The rod may be advantageously adapted to mount withrespect to an upwardly-extending structure associated with a pediclescrew. The rod/pedicle screw may be mounted with respect to each othersuch that relative movement of the rod relative to the pedicle screw ispermitted in at least one plane.

In a still further embodiment, a method is disclosed for producing aspring junction in which a resilient element is welded to a structuralmember such that an active region of the resilient element is disposedphysically separately with respect to the heat-affected zone associatedwith such welding. In some such embodiments, a further step is disclosedin which a resilient element is provided that defines an active regionand a bend region, and wherein such welding results in the bend regionbeing disposed between the active region and the heat-affected zone.Such a resilient element can include a coil extending along ahelically-shaped path, and in which the bend region is configured so asto initially bend away from such helical path defined before bendingback toward such helical path.

In a still further embodiment, a combination is provided that includes astructural member having a first end, a second end opposite the firstend, an aperture between the first end and the second end, and a notchformed in the second end. The combination also includes a resilientelement having a bend region at an end thereof, the bend regionterminating at a termination. The resilient element is secured to thefirst end of the structural member such that the bend region extendsthrough the aperture and the termination is lodged in the notch. In somesuch embodiments, the resilient element is further affixed to thestructural member via a weld formed with respect to the termination andthe structural member at the notch. In other such embodiments, thetermination is configured and dimensioned so as to extend at leastpartially in the direction of the first end of the structural member,and the bend region is configured and dimensioned such that thetermination can be threaded through the aperture, and thereby rotatedtoward and into the notch. In some such cases the structural memberincludes a helical groove formed in the first end and terminatingadjacent the aperture, and the resilient element includes an activeregion adjacent the bend region and spaced apart from the termination,and the active region includes a coil threaded along the helical grooveto an extent of the aperture.

The spring junction(s) of the present disclosure are typically employedas part of a spinal stabilization system that may advantageously includeone or more of the following structural and/or functional attributes:

-   -   Exemplary embodiments of the spring junction (and associated        spring/structural member subassembly) are capable of undergoing        at least approximately 10,000,000 cycles of combined        extension/contraction and bending (e.g., during mechanical        testing);    -   Implementation of the disclosed spring junctions have no        substantial effect on the footprint of the dynamic stabilization        devices in which they are incorporated, e.g., the resilient        elements (e.g., springs) of such spinal stabilization devices do        not extend radially inwardly or outwardly to a greater extent        than the dynamic stabilization devices that do not include the        disclosed spring junctions, thereby preserving compatibility        with existing components and/or proven or preferred geometries;    -   An outwardly/upwardly, then inwardly/downwardly extending bend        region at each end of the resilient element, combined with a        notch on the external end of each spring cap plate provides a        snap-fit system which positively locates the ends of the        resilient element within their respective notches during        pre-welding assembly, and presents a convenient face for        purposes of electronic-beam welding without undue risk of        annealing and/or other types of damage to the active region of        the resilient element.

Advantageous spine stabilization devices, systems and methods mayincorporate one or more of the foregoing structural and/or functionalattributes. Thus, it is contemplated that a system, device and/or methodmay utilize only one of the advantageous structures/functions set forthabove, a plurality of the advantageous structures/functions describedherein, or all of the foregoing structures/functions, without departingfrom the spirit or scope of the present disclosure. Stated differently,each of the structures and functions described herein is believed tooffer benefits, e.g., clinical advantages to clinicians and/or patients,whether used alone or in combination with others of the disclosedstructures/functions.

Additional advantageous features and functions associated with thedevices, systems and methods of the present disclosure will be apparentto persons skilled in the art from the detailed description whichfollows, particularly when read in conjunction with the figures appendedhereto. Such additional features and functions, including the structuraland mechanistic characteristics associated therewith, are expresslyencompassed within the scope of the present invention.

BRIEF DESCRIPTION OF THE DRAWINGS

To assist those of ordinary skill in the art in making and using thedisclosed devices, systems and methods for achieving enhancedreliability, dependability, and/or durability, e.g., in a dynamic spinalstabilization device, reference is made to the appended figures wherein:

FIG. 1 is a perspective exploded assembly view of a spinal stabilizationdevice/system, according to the present disclosure;

FIG. 2 is an exploded assembly view of a spinal stabilizationdevice/system, including pedicle screws and associated mountingstructures, in accordance with an embodiment of the present disclosure;

FIG. 3 is an unexploded assembly view of the exemplary spinalstabilization device/system of FIG. 2;

FIGS. 4, 5 and 6 are interior end, exterior end, and cross-sectionalviews of a structural member associated with the exemplary spinalstabilization device/system of FIGS. 2-3;

FIGS. 7, 8 and 9 are interior end, exterior end, and cross sectionalviews of another structural member associated with exemplary spinalstabilization device/system of FIGS. 2-3;

FIG. 10 is a side view of a resilient element that may be employed informing one or more spring junctions according to the presentdisclosure;

FIG. 11 is a side assembly view of the exemplary spinal stabilizationdevice/system of

FIGS. 2-3 illustrating assembly of the components of FIGS. 4-9;

FIG. 12 is a perspective detail view of the interface between thestructural member of FIGS. 7-9 and the resilient element of FIG. 10;

FIG. 13 is a top view of the interface between the structural member ofFIGS. 7-9 and the resilient element of FIG. 10;

FIG. 14 is a sectional view of the interface between the structuralmember of FIGS. 7-9 and the resilient element of FIG. 10 taken along theline 14-14 of FIG. 13; and

FIGS. 15 and 16 illustrate various exemplary types and ranges of motionassociated with exemplary spinal stabilization devices/assemblies of thepresent disclosure.

DESCRIPTION OF EXEMPLARY EMBODIMENTS

The present disclosure provides advantageous devices, systems andmethods for improving the reliability, dependability and/or durabilityof spinal stabilization systems. More particularly, the presentdisclosure provides advantageous devices, systems and methods formechanically mounting resilient elements (e.g., torsion springs and/orcoil springs) to, and/or for coupling resilient elements between,structural members (e.g., plates, caps, flanges, rods, and/or bars)associated with dynamic spinal stabilization systems. The mountingand/or coupling methods/techniques of the present disclosure provideenhanced reliability, dependability and/or durability withoutsignificantly increasing material weight or volume requirements andwithout compromising the important functions of the dynamic spinalstabilization devices/systems of which they form a part.

The exemplary embodiments disclosed herein are illustrative of theadvantageous spinal stabilization devices/systems and surgical implantsof the present disclosure, and of methods/techniques for implementationthereof. It should be understood, however, that the disclosedembodiments are merely exemplary of the present invention, which may beembodied in various forms. Therefore, the details disclosed herein withreference to exemplary dynamic spinal stabilization systems andassociated methods/techniques of assembly and use are not to beinterpreted as limiting, but merely as the basis for teaching oneskilled in the art how to make and use the advantageous dynamic spinalstabilization systems and alternative surgical implants of the presentdisclosure.

With reference to FIG. 1, components of a dynamic stabilization element10 disclosed in commonly assigned U.S. Non-Provisional patentapplication Ser. No. 11/027,270, filed Dec. 31, 2004 (hereinafter “the'270 Application”), are shown in an exploded view. The disclosure of the'270 Application is hereby incorporated herein by reference in itsentirety. As shown in FIG. 1, the dynamic stabilization element 10includes two structural elements in the form of a spring cap 12 and aspring cap 14, and two resilient elements in the form of an inner spring16 and an outer spring 18. The spring cap 12 is affixed to an attachmentmember 20 that is configured to be coupled to the head of a pediclescrew (not shown) via a dynamic joint (not shown). The spring cap 14 isaffixed to a rod 22 that is configured to be attached to anotherattachment member (not shown) that is in turn coupled to the head ofanother pedicle screw (not shown) via another dynamic joint (not shown).The dynamic stabilization element 10 permits relative axial/longitudinalmotion, as well as angular/rotational motion, of the rod 20 relative tothe attachment member 20, as part of a larger spinal stabilizationsystem (shown only in relevant part).

The spring cap 12 includes an interior end 24, an exterior end 26opposite the interior end, a post 28 axially positioned on the interiorend 24, an annular channel 30 formed in the interior end 24 around thepost 28, a helically-shaped groove 32 formed in the interior end 24around the annular channel 30, and an aperture 34 passing through thespring cap 12 between the interior and exterior ends 24, 26 thereof atan end 36 of the helically-shaped groove 32. The spring cap 14 includesan interior end 38, an exterior end 40 opposite the interior end 38, apost 42 axially positioned on the interior end 38 around the post 42, ahelically-shaped groove 46 formed in the interior end 38 around theannular channel 44, and an aperture 48 passing through the spring cap 14between the interior and exterior ends 38, 40 thereof at an end 50 ofthe helically-shaped groove 46.

The inner spring 16 consists of coils 52 sharing a common diameter andarranged sequentially about a common axis between a coil termination 54(obscured) at an end 56 of the inner spring 16 and a coil termination 58at another end 60 thereof opposite the end 56. The outer spring 18consists of coils 62 sharing a common diameter and arranged sequentiallyabout a common axis between a coil termination 64 (obscured) at an end66 of the outer spring 18 and a coil termination 68 at another end 70thereof opposite the end 66.

In the assembled state of the dynamic stabilization element 10, theinner spring 16 is positioned within the outer spring 18. The coil 52 atthe end 56 of the inner spring 16 is positioned on or around the post 28of the spring cap 12, and against the interior end 24 of the spring cap12 so as to occupy (at least in part) the annular channel 30 formedtherein. The coil 52 at the end 60 of the inner spring 16 is positionedon or around the post 42 of the spring cap 14 and against the interiorend 38 of the spring cap 14 so as to occupy (at least in part) theannular channel 44 formed therein. In this way, the inner spring 16 iseffectively captured between the spring cap 12 and the spring cap 14 andeffectively floats relative to the opposing posts 28, 42. The coil 62 atthe end 66 of the outer spring 18 is threaded into the interior end 24of the spring cap 12 along the helically-shaped groove 32 at least untilthe coil termination 64 reaches the aperture 34 of the spring cap 12.The outer spring 18 is fixed with respect to the spring cap 12, e.g., bywelding, and may be trimmed so as to be flush relative to an edge formedat the interface between the aperture 34 and the exterior end 26 of thespring cap 12. The coil 62 at the end 70 of the outer spring 18 isthreaded into the interior end 38 of the spring cap 14 along thehelically-shaped groove 46 at least until the coil termination 68reaches the aperture 48 of the spring cap 14. The outer spring 18 isfixed with respect to the spring cap 14, e.g., by welding, and may betrimmed so as to be flush relative to an edge formed at the interfacebetween the aperture 48 and the exterior end 40 of the spring cap 14.

As described in the '270 Application, the outer spring 18 is typicallyshorter than the inner spring 16, such that as the spring cap 12 and thespring cap 14 are brought toward each other (i.e., to permit the outerspring 18 to be mounted on both), the inner spring 16 is placed incompression. The degree to which the inner spring 16 is compressed isgenerally dependent on the difference in length as between the inner andouter springs 16, 18. Thus, the preload compression of the inner spring16 may be controlled and/or adjusted in part through selection of therelative lengths of the inner and outer springs 16, 18. In addition tothe preload compression of the inner spring 16, the mounting of theouter spring 18 with respect to the spring caps 12, 14 includes placingthe outer spring 18 in tension. The overall preload of the dynamicstabilization element 10 corresponds to equal and opposite forcesexperienced by and/or contained within the inner and outer springs 16,18.

The inner spring 16 reaches its free length (i.e., non compressed state)at or about the point at which a patient's movement exceeds a “neutralzone” (as described more completely in the '270 Application). Beyondthis point, the inner spring 16 is free floating (e.g., on the opposingposts 28, 42), while the outer spring 18, already in tension, extends inlength even further.

In the overall design of the disclosed spinal stabilization system,optimization of the attachment between the outer spring 18 and thespring cap 14 is desirable. In experimental studies associated withspinal stabilization devices of the type disclosed herein, it has beennoted that direct welding of the outer spring 18 and the spring cap 14may not provide an optimal means of attachment. While not intending tobe bound by theory, it is believed that a “heat-affected” zone may becreated in the coil 62 at the end 70 of the outer spring 18 as a resultof the process of welding the outer spring 18 to the spring cap 14. Moreparticularly, such heat-affected zone is believed to arise as a resultof an annealing effect brought about by the migration of excess heatarising from an electronic-beam welding process. In accordance with suchelectronic beam or E-beam welding processes, elevated temperatures in arange of approximately 1000° F. or higher are used to affix the outerspring 18 to the spring cap 14 by essentially melting such componentstogether. The heat-affected zone so produced can be at least0.005″-0.030″ in axial length, and is located immediately adjacent theweld formed at the end 70 of the outer spring 18, and along the activeregion of the outer spring 18. (As used herein in reference to a springor resilient element, the term “active region” or “active portion”refers to a region, portion, or part of the spring or resilient elementwhich, during normal in-situ use and/or representative mechanicaltesting of the spring or resilient element, actively contributes to thecharacteristic stiffness of the spring or resilient element, and/oractively participates in the axial travel and/or lateral bendingthereof.) The heat-affected zone can include a soft or weak point on thecoil 62 at which a Rockwell hardness of the material of the outer spring18, ordinarily falling within a range of from approximately 46 toapproximately 54, dips sharply; e.g., to a value in a range of fromapproximately 20 to approximately 24.

According to the present disclosure, geometric/structural modificationsto the outer spring 18 and the spring cap 14 have been found toadvantageously enhance the reliability and durability of dynamicstabilization element 10. Exemplary embodiments of the advantageousgeometric/structural modifications to the outer spring 18 and the springcap 14 are described hereinbelow with reference to FIGS. 2-14, as is abeneficial cooling/supercooling step involving the modified outer springand the modified spring caps associated therewith. As a result of thesegeometric/structural modifications, and/or of the cooling/supercoolingstep, a durability standard of 10,000,000+failure-free cycles has beenachieved with apparatus in which an outer spring has been welded to itsassociated spring caps to form a dynamic stabilization device asdescribed herein.

According to exemplary embodiments of the present disclosure, thegeometric/structural modifications include the creation of a substantialphysical separation of the active portion of the outer spring from theheat-affected zone associated with the E-beam welding process, and/orfrom the actual site of the weld formed between the attached components.As a result of this separation, to the extent that any region of theouter spring becomes significantly annealed, and/or is brought to asignificantly lowered Rockwell hardness value as a result of E-beamwelding, the amount of cyclic stress to which that softened or annealedportion is exposed is substantially reduced and/or brought to such a lowlevel that the respective junctions between the outer spring and itsassociated spring caps can exhibit very high levels ofreliability/durability.

With reference to FIGS. 2 and 3, a dynamic spinal stabilization system100 is shown in accordance with an exemplary embodiment of the presentdisclosure. Referring to FIG. 2, the spinal stabilization system 100includes attachment members 102, 104, pedicle screws 106, 108,ball/spherical elements 110, 112, and set screws 114, 116. Theattachment member 102 is configured to receive the ball/sphericalelement 110. The ball/spherical element 110 then receives the head ofthe pedicle screw 106 such that a global/dynamic joint is formed betweenthe attachment member 102 and the head of the pedicle screw 106 (seealso FIG. 3). The set screw 114 is then inserted into the head of thepedicle screw 106 (see also FIG. 3), thereby securing the head of thepedicle screw 106 within the ball/spherical element 110. The attachmentmember 104 is configured to receive the ball/spherical element 112. Theball/spherical element 112 then receives the head of the pedicle screw108 such that a global/dynamic joint is formed between the attachmentmember 104 and the head of the pedicle screw 108 (see also FIG. 3). Theset screw 116 is then inserted into the head of the pedicle screw 108(see also FIG. 3), thereby securing the head of the pedicle screw 108within the ball/spherical element 112.

The spinal stabilization system 100 also includes a rod 118. The rod isconfigured to be inserted into the attachment member 104, which includesa transverse aperture 120 to accommodate the rod 118, and a set screw122 to secure the rod 118 at a desired position within the transverseaperture 120 (see also FIG. 3, in which a hex driver 124 is shownturning the set screw 122 against the rod 118).

The spinal stabilization system 100 further includes a dynamicstabilization element 126 between the rod 118 and the attachment member102. The dynamic stabilization element 126 includes structural members128, 130, an inner resilient element 132, an outer resilient element134, a sheath member 136, and two end clamps 138. As shown in FIG. 3,the inner resilient element 132 (obscured) and outer resilient element134 (partially obscured) are positioned within the sheath member 136,and an end clamp 138 secures the sheath member 136 to each of thestructural members 128, 130. This prevents undesirable interaction orinterference between the inner and outer resilient elements 132, 134 andanatomical structures in situ. Referring again to FIG. 2, the innerresilient element 132 is constructed and functions in mannerssubstantially similar to those of the inner spring 16 describedhereinabove with reference to the dynamic stabilization element 10. Theinner resilient element 132 is also deployed and employed in the dynamicstabilization element 126 in manners substantially similar to those inwhich the inner spring 16 is deployed and employed in the dynamicstabilization element 10 described hereinabove.

The following components of the dynamic stabilization element 126 willnow be described in greater detail: the structural member 128 (withreference to FIGS. 4-6), the structural member 130 (with reference toFIGS. 7-9), and the outer resilient element 134 (with reference to FIG.10). Next, the manner in which the structural members 128, 130 and theouter resilient element 134 are assembled will be discussed (withparticular reference to FIGS. 11-14). Then, the functions of the dynamicstabilization element 126 will be discussed, followed by a discussion ofthe characteristic advantages of the dynamic stabilization element 126.

Referring now to FIGS. 4-6, the structural member 128 is affixed to(e.g., is of unitary construction with) the attachment member 102 (theball/spherical element 110 is also shown within the attachment member102) and takes the form of a plate having multiple features permittingthe structural member 128 to function in the manner of an end cap orspring cap with respect to the inner and outer resilient elements 132,134 (FIG. 2). The structural member 128 includes an interior end 140, anexterior end 142 opposite the interior end 140, a post 143 axiallypositioned on the interior end 140, an annular channel 144 formed in theinterior end 140 around the post 143, a helically-shaped groove 146formed in the interior end 140 around the annular channel 144, anaperture 148 passing through the structural member 128 between theinterior and exterior ends 140, 142 thereof at an end 150 of thehelically-shaped groove 146, a short groove 152 formed in the exteriorend 142 adjacent the aperture 148, and a notch 154 formed in theexterior end 142 at an end 156 of the short groove 152. The structureand function of the structural member 128 will be described in greaterdetail hereinafter.

Referring now to FIGS. 7-9, the structural member 130 is affixed to(e.g., is of unitary construction with) the rod 118 (which is positionedoff-axis or off-center with respect to the structural member 130), andtakes the form of a plate having multiple features permitting thestructural member 130 to function in the manner of an end cap or springcap with respect to the inner and outer resilient elements 132, 134(FIG. 2). The structural member 130 includes an interior end 158, anexterior end 160 opposite the interior end 158, a post 162 axiallypositioned on the interior end 158, an annular channel 164 formed in theinterior end 158 around the post 162, a helically-shaped groove 166formed in the interior end 158 around the annular channel 164, anaperture 168 passing through the structural member 130 between theinterior and exterior ends 158, 160 thereof at an end 170 of thehelically-shaped groove 166, a short groove 172 formed in the exteriorend 160 adjacent the aperture 168, and a notch 174 formed in theexterior end 160 at an end 176 of the short groove 172. The structureand function of the structural member 130 will be described in greaterdetail hereinafter.

Referring now to FIG. 10, the outer resilient element 134 consists ofcoils 178 sharing a common diameter and arranged sequentially about acommon axis between a coil termination 180 at an end 182 of the outerresilient element 134 and a coil termination 184 at another end 186thereof opposite the end 182. Extending from the coil termination 180,and substantially continuous therewith, is a bend region 188 of theouter resilient element 134. Extending from the coil termination 184,and substantially continuous therewith, is a bend region 190 of theouter resilient element 134.

The bend regions 188, 190 of the outer resilient element 134 extendperipherally from the respective coil terminations 180, 184 alongrespective paths which, when viewed axially (see, e.g., FIG. 13) fromeither end 182, 186 of the outer resilient element 134, are defined byrespective single radii that extend from the common axis of the coils178 of the outer resilient element 134 and that have extentsapproximately half that of the common diameter of the coils 178. As aresult, the bend regions 188, 190 of the outer resilient element 134remain within the same peripheral outline defined by the coils 178 ofthe outer resilient element 134. When viewed from the side, however, asin FIG. 10, the bend regions 188, 190 of the outer resilient element 134are seen to depart from the helical path defined by the coils 178.

More particularly, the bend region 188, when viewed from the side as inFIG. 10, is seen to include a curve or bend in the path of extension ofthe bend region 188, according to which the material of the outerresilient element 134: (1) initially curves away from the adjacent coil178 at the coil termination 180; (2) reaches an apex 192 representing apoint of maximum departure from the adjacent coil 178; (3) curvestherefrom back toward the adjacent coil 178; and (4) terminates at abend region termination 194 without fully returning to the helical pathdefined by the coils 178. Also, the bend region 190, when viewed fromthe side as in FIG. 10, is seen to include a curve or bend in the pathof extension of the bend region 190, according to which the material ofthe outer resilient element 134: (1) initially curves away from theadjacent coil 178 at the coil termination 184; (2) reaches an apex 196representing a point of maximum departure from the adjacent coil 178;(3) curves therefrom back toward the adjacent coil 178; and (4)terminates at a bend region termination 198 without fully returning tothe helical path defined by the coils 178. The structure and function ofthe outer resilient element 134 will be described in greater detailhereinafter.

In the assembled state of the dynamic stabilization element 126 shown inFIG. 11, the inner resilient element 132 (obscured, see FIG. 2) ispositioned within the outer resilient element 134, between therespective posts 143 (FIG. 4), 162 (FIG. 7), and within the respectiveannular channels 146 (FIG. 4), 164 (FIG. 7) of the structural elements128, 130. The bend region 190 and the coil 178 at the end 186 (FIG. 10)of the outer resilient element 134 are threaded into the interior end140 (FIG. 6) of the structural element 128 until the bend region 190 hassubstantially passed into or through the aperture 148 of the structuralelement 128 and the bend region termination 198 has been caused to dropor snap into place within the notch 154 (FIG. 5) formed in the exteriorend 142 of the structural element 128. The bend region 188 and the coil178 at the end 182 (FIG. 10) of the outer resilient element 134 arethreaded into the interior end 158 (FIG. 9) of the structural element130 until the bend region 188 has substantially passed into or throughthe aperture 168 of the structural element 130 and the bend regiontermination 194 (obscured, see FIG. 10) has been caused to drop or snapinto place within the notch 174 (FIG. 8) formed in the exterior end 160of the structural element 130.

Referring now to FIG. 12, the interface or spring junction between theouter resilient element 134 and the structural element 130 is shown ingreater detail. As indicated above, the bend region 188 largely orcompletely extends into or through the aperture 168 formed in thestructural element 130, and the bend region termination 194 is lodgedwithin the notch 174 formed in the exterior end 160 of the structuralelement 130. More particularly, a portion 200 of the bend region 188 ofthe outer resilient element 134 near the coil termination 180 is lodgedwithin the short groove 172 (FIG. 9) formed in the exterior end 160 ofthe structural element 130, a portion 202 of the bend region 188associated with the apex 192 thereof is lodged within the short groove172 and in longitudinal contact with the exterior end 160 of thestructural element 130, and a portion 204 of the bend region 188associated with the bend region termination 194 is lodged within theshort groove 172 to an extent of the notch 174. The outer resilientelement 134 is welded to the exterior end 160 of the structural element130 in the vicinity of the notch 174, e.g., via electronic-beam weldingalong an extent of the portion 204 of the bend region 188 that is lodgedwithin the notch 174. The outer resilient element 134 can be placed in astate of full compression in advance of such welding so as to ensurethat after such welding, the portion 202 of the bend region 188associated with the apex 192 thereof is biased in favor of continuouslongitudinal contact with the exterior end 160 of the structural element130 during normal in situ use of, and/or during representativemechanical testing of, the dynamic stabilization element 126.

Though not shown in FIG. 12, a portion (not separately shown) of thebend region 190 (FIG. 10) near the coil termination 184 (FIG. 10) issimilarly lodged within the short groove 152 (FIG. 5) formed in theexterior end 142 (FIG. 6) of the structural element 128, a portion (notseparately shown) of the bend region 190 (FIG. 10) associated with theapex 196 (FIG. 10) thereof is lodged within the short groove 152 and inlongitudinal contact with the exterior end 142 of the structural element128, and a portion (not separately shown) of the bend region 190associated with the bend region termination 198 is lodged within theshort groove 152 to an extent of the notch 154. The outer resilientelement 134 is welded to the exterior end 142 of the structural element128 in the vicinity of the notch 154, e.g., via electronic-beam weldingalong an extent of the portion (not separately shown) of the bend region190 that is lodged within the notch 154 (FIG. 5). The outer resilientelement 134 can be placed in a state of full compression in advance ofsuch welding for the same reasons and to achieve a similar biasingeffect in the bend region 190 as is described above with reference tothe bend region 188.

A cooling/supercooling step may be advantageously undertaken in advanceof welding such as is described immediately hereinabove. In accordancewith such a step, the outer resilient element 134 and the structuralmembers 128, 130 are immersed in a bath of liquid nitrogen, and arewithdrawn therefrom shortly before the resilient element 134 is weldedto the structural elements 128, 130. Cooling/supercooling of the outerresilient element 134 and the structural members 128, 130 functions toreduce the likelihood that high levels of heat will be experienced at adistance from the respective weld regions associated therewith.Accordingly, a given heat-affected zone associated with the migration ofheat generated by electronic beam welding can be shrunken and/or reducedin extent, as can any soft or weak spot in such heat-affected zoneassociated with sharply reduced Rockwell hardness. Thiscooling/supercooling step was observed to increase resilient elementdurability during representative mechanical testing.

Referring to FIGS. 13 and 14, the above-described welding processproduces a weld region 206 incorporating portions of the exterior end160 of the structural element 130 at the end 176 of the short groove 172in the vicinity of the notch 174, as well as portions of the bendtermination 194 of the bend region 188 of the outer resilient element134. The portion 204 of the bend region 188 is long enough, and thecorresponding portion of the short groove 172 is long enough, such thatweld region 206 terminates at a point 208 along the extent of the bendregion 188 well short of the apex 192 thereof Accordingly, the weldregion 206 also terminates well short of a corresponding apex 210 of theshort groove 172 against which the portion 202 of the bend region 188 isbiased. To the extent the portion 204 of the bend region 188 includes aheat-affected zone 212 associated with the process used to affix theouter resilient element 134 to the structural element 130, such region212 also terminates at a point 214 along the extent of the bend region188 well short of the apex 192 thereof, as well as well short of theapex 210 of the short groove 172. The portion 202 of the bend region 188and the exterior end 160 of the structural member 130 are in intimateand continuous longitudinal contact along the short groove 172 at leastfrom the apex 210 thereof and for an extent 216 extending toward theaperture 168. Beyond the extent 216, the short groove 172 tends todepart from intimate contact from the portion 200 of the bend region 188for an extent 218 extending fully to the aperture 168. The significanceand functional benefits of such structure and/or such assemblyarrangement between the bend region 188 of the outer resilient element134 and the exterior end 160 of the structural element 130 will beexplained more fully hereinafter.

Turning now to FIGS. 15 and 16, in operation, the dynamic stabilizationelement 126 of the spinal stabilization system 100 (FIG. 2) permitsrelative rotational motion, as well as relative translational motion, asbetween the rod 118 and the attachment member 102, and/or as between therod 118 and the ball/spherical element 110, while providing enhancedspinal support for the patient, e.g., in the “neutral zone” describedmore fully in the ‘270 Application. More particularly, the dynamicstabilization element 126 as a unit, and/or the outer resilient element134 by itself, supports either and/or both of spinal extension andspinal flexion. Referring to FIG. 15, the dynamic stabilization element126 is shown as it would appear while supporting spinal extension,wherein an extent 220 of, for example, less than 5° of relative rotationas between the rod 118 and the ball/spherical element 110 is produced.Such spinal extension can also produce approximately one millimeter oftravel in the resilient element 134 relative to the initial positionthereof (i.e., wherein the resilient element 134 is preloaded in tensionso as to be slightly extended), such that the resilient element 134 maynow actually assume a fully compressed state. Referring to FIG. 16, thedynamic stabilization element 126 is shown as it would appear whilesupporting spinal flexion, wherein an extent 222 of, for example,greater than 10° of relative rotation as between the rod 118 and theball/spherical element 110 is produced. Such spinal flexion can produceapproximately one and one-half millimeters of travel (i.e., additionalextension) in the resilient element 134 relative to the initial positionthereof.

Referring again to FIG. 14, the outer resilient element 134 is shown ina state of full compression against the interior end 158 of thestructural element 130. As discussed above, when the outer resilientelement 134 is in this condition, the bend region 188 of the outerresilient element 134 is biased toward contact with the exterior end 160of the structural element 130. To the extent the outer resilient element134 is caused to expand from its fully compressed state, this bias isnot relaxed. Rather, this bias is only reinforced by such torsionaland/or bending forces as may tend to urge the portion 200 of the bendregion 188 further through the aperture 168 in the direction of theinterior end 158. (For example, depending on the particular axial and/orlateral forces imposed upon the outer resilient element 134, the portion200 of the bend region 188 can tend to bend and/or twist close to/closerto the angled exterior surface associated with the extent 218 of theshort groove 172). At the same time, the portion 202 of the bend region188 remains lodged in the short groove 172, where it remains in intimatecontact with the exterior end 160 of structural element 130, and as suchis not capable of being deflected any further in the direction of theinterior end 158 by such axial and/or lateral forces. Accordingly, suchaxial and/or lateral forces are prevented from directly acting uponeither of the weld region 206 or the heat-affected zone 212 of the outerresilient element 134. More particularly, the consistent, continuouslongitudinal contact between the portion 202 of the bend region 188 andthe exterior end 160 of the structural element 130 along the shortgroove 172 thereof acts as a permanent ‘fulcrum’, beyond which thetorsional and/or bending forces arising in the portion 200 of the bendregion 188 are not necessarily transmitted as such to the weld region206 or the heat-affected zone 212, at least not in a form capable ofproducing fatigue-inducing stress in such region/zone. In other words,the active region of the outer resilient element 134 extends no furthertoward the weld region 206 or the heat-affected zone 212 than the apex192 of the bend region 188. Since such regions are physically separatedfrom the apex 192 via corresponding structural features of the outerresilient element 134 and the structural member 130, and/or via themanner in which the same are affixed to each other, such forces as areapplied to the weld region 206 and the heat-affected zone 212 during insitu use or representative mechanical testing will have been channeledinto a cantilevered arrangement. In accordance with such cantileveredarrangement, a fulcrum (e.g., the extent 216 within the short groove172) provides the weld region 206 with significant mechanical advantageby which to resist such forces without experiencing undue internalstress.

The dynamic stabilization element 126 associated with the spinalstabilization system 100 described hereinabove with regard to FIGS. 2-14provides numerous advantages in comparison to other spinal stabilizationsystems associated therewith. Referring again to FIGS. 11 and 14, andwhile not necessarily intending to be bound by theory, improvedreliability and durability is achieved with the disclosed dynamicstabilization element based at least in part on the fact that theheat-affected zone associated with the process of joining the outerresilient element 134 to the structural elements 128, 130 via welding isphysically separated from the active region of the outer resilientelement 134, and is therefore isolated from the cyclical stressassociated with repeated extension/contraction and/or bending duringnormal use and/or representative mechanical testing. More particularly,the portion 202 of the bend region 188 of the outer resilient element134 fully separates the portion 202 of the outer resilient element 134from the portion 204 thereof at which the outer resilient element 134 iswelded to the structural member 130. In like measure, and in a similarfashion, the welded and threaded connection between the outer resilientelement 134 and the structural member 128 provides similar advantages.Typically, due to the particular structures and assembly methodsdescribed above, the heat-affected zone in exemplary embodiments of thepresent disclosure is observed to extend axially approximately005″-0.030″ from the weld region along the material of the outerresilient element 134, and the active region of the outer resilientelement 134 extends no farther in the direction of the welded interfacesthan the respective apexes 192, 196 of the bend regions 188, 190. Sincethe bend regions 188, 190 are each approximately 0.150 inches in length,the increased reliability/durability found in the dynamic stabilizationelement of the present disclosure has been shown to be at leastpartially due to the fact that the active region of the outer resilientelement 134 is substantially completely shielded from any materialdegradation that may result from the assembly step, e.g., viaelectronic-beam welding. In other words, to the extent the use of E-beamwelding reduces the Rockwell hardness of a portion or portions of theouter resilient element 134, such portion or portions are substantiallycompletely shielded from fatigue-producing levels of cyclic stress.

The dynamic stabilization element 126 associated with the spinalstabilization system 100 described hereinabove with regard to FIGS. 2-14can be the subject of numerous modifications and variations while stillexhibiting the above-discussed advantages over other dynamic junctionsfor spinal stabilization systems. For example, the rod 118 can berepositioned to an axial position with respect to the structural member130. The bend region termination 194 can be affixed to the structuralmember 130 by other welding processes than E-beam welding, and/or by oneor more non-welding means of attachment, such as by clamping or the useof mechanical fasteners appropriate for use in conjunction with smallgage springs, by an adhesive-based process, or via the use of a singlemold to form the two components together as a single piece. To theextent such attachment schemes result in respective attachment regionsalong which the bend region termination 194 is affixed to the structuralmember, such attachment regions are similarly disposed physicallyseparately relative to the respective active region of the outerresilient element 134 s (whether or not heat-affected zones arepresent), and are thereby similarly shielded from the types and levelsof cyclical stress known to produce fatigue failure. The outer resilientelement 134 need not necessarily be configured in the manner of a coilspring, but may instead take the form of one or more other types ofresilient elements, such as a leaf spring, a torsion spring or bar, etc.Additionally, the outer resilient element 134 may be employed in adynamic junction that does not also include the inner resilient element132. Many other variations and/or modifications are possible.

Although the present disclosure has been disclosed with reference toexemplary embodiments and implementations thereof, those skilled in theart will appreciate that the present disclosure is susceptible tovarious modifications, refinements and/or implementations withoutdeparting from the spirit or scope of the present invention. In fact, itis contemplated the disclosed connection structure may be employed in avariety of environments and clinical settings without departing from thespirit or scope of the present invention. Accordingly, while exemplaryembodiments of the present disclosure have been shown and described, itwill be understood that there is no intent to limit the invention bysuch disclosure, but rather, the present invention is intended to coverand encompass all modifications and alternate constructions fallingwithin the spirit and scope hereof.

1. A spinal stabilization element, comprising: (a) a spring cap; (b) anattachment member that is structurally associated with the spring cap,said attachment member being substantially transversely orientedrelative to the spring cap and adapted to be mounted with respect to afirst pedicle screw; and (c) a resilient element that includes a bendtermination at an end thereof, wherein said bend termination of saidresilient element and said spring cap are integrally formed.
 2. Thespinal stabilization element according to claim 1, wherein saidresilient element defines a central axis and wherein said attachmentmember is offset from said central axis.
 3. The spinal stabilizationelement according to claim 1, wherein said spring cap defines aninterior end and an exterior end, and wherein said resilient element isflush relative to the exterior end of the spring cap.
 4. The spinalstabilization element according to claim 1, wherein said resilientelement is selected from the group consisting of a coil spring, a leafspring, a torsion spring and a torsion bar.
 5. The spinal stabilizationelement according to claim 1, wherein said resilient element defines asecond end opposite said bend termination and a central axis, andwherein said bend termination and said second end of said resilientelement are spaced from one another along said axis.
 6. The spinalstabilization element according to claim 5, wherein said resilientelement is compressible and extendable along said axis.
 7. Incombination: (a) a first element including: (i) a first spring cap; (ii)an attachment member that is structurally associated with the firstspring cap, said attachment member being substantially transverselyoriented relative to the first spring cap and adapted to be mounted withrespect to a pedicle screw; and (iii) a resilient element that includesa bend termination at an end thereof, wherein said bend termination ofsaid resilient element and said first spring cap are integrally formed;and (b) a second element including a second spring cap in spacedrelation relative to the bend termination of said resilient element andconfigured to be mounted with respect to a second pedicle screw.
 8. Thecombination according to claim 7, wherein said resilient element definesa central axis and wherein said attachment member of said first springcap is offset from said central axis.
 9. The combination according toclaim 7, wherein said resilient element defines a second end and saidsecond end of said resilient element is operatively coupled to saidsecond spring cap.
 10. The combination according to claim 7, whereinsaid resilient element defines an axis, said first and second ends ofsaid resilient element are spaced from one another along said axis, andsaid resilient element is compressible and extendable along said axis.11. The combination according to claim 7, wherein said resilient elementis selected from the group consisting of a coil spring, a leaf spring, atorsion spring and a torsion bar.
 12. A spinal stabilization systemcomprising: (a) first and second pedicle screw; (b) a first elementincluding: (i) a first spring cap; (ii) an attachment member that isstructurally associated with the first spring cap, said attachmentmember being substantially transversely oriented relative to the firstspring cap and adapted to be mounted with respect to a pedicle screw;and (iii) a resilient element that includes a bend termination at an endthereof, wherein said bend termination of said resilient element andsaid first spring cap are integrally formed; and (c) a second elementincluding a second spring cap in spaced relation relative to the bendtermination of said resilient element and configured to be mounted withrespect to a second pedicle screw.
 13. The spinal stabilization systemaccording to claim 12, wherein said resilient element is selected fromthe group consisting of a coil spring, a leaf spring, a torsion springand a torsion bar.